Production method and apparatus



April 8, 1953 F. s. TUTTON PRODUCTION METHOD AND APPARATUS l3 Sheets-Sheet 1 Filed Dec. 27, 1946 ,ZZ/JKMM INVENTOR Min April 28, 1953 F. s. TUTTON 2,636,445

PRODUCTION METHOD AND APPARATUS Filed Dec. 27, 1946 13 Sheets-Sheet 3 April 28, 1953 F. s. TUTTON 2,636,445

PRODUCTION METHOD AND APPARATUS Filed Dec. 27, 1946 13 Sheets-Sheet 4 3/4 all are 32,1 a/z 3/6 aza- i so:

326 I so; an 3Z7 jam FIG. l6 of at ya; Z

AUG/MEX! April 28, 1953 F. s. TUTTON PRODUCTION METHOD AND APPARATUS l3 Sheets-Sheet 5 Filed Dec. 27, 1946 Fl G.22

FIG.23

FIG.2O

INVENTOR BY {W ATEORNEYJ FIDG. l9

- April 28, 1953 s, TUTTON 2,636,445

PRODUCTION METHOD AND APPARATUS Filed Dec. 27, 1946 13 Sheets-Sheet 6 BY%%M A TORNEYS.

April 1953 F. s. TUTTON 2,636,445

PRODUCTION METHOD AND APPARATUS Filed Dec. 27, 1946 15 Sheets-Sheet 7 i u v I i m 1 I 513 FIG. 28

INVE'NTOR BY I ATTORN EYS.

April 28, 1953 F. s. TUTTON 2,636,445

PRODUCTION METHOD AND APPARATUS Filed Dec. 27, 1946 15 Sheets-Sheet 9 O if? n W, i

ATTORN EYJ April 28, 1953 F. s. TUTTON PRODUCTION METHOD AND APPARATUS l3 Sheets-Sheet 10 Filed Dec. 27, 1946 diam.

INVENTOR w BY A TORNEYsS April 28, 1953 F. s; TUTTON PRODUCTION AND APPARATUS 1s Sheets-'She et'H Filed Dec 27, 1946 aid/M4,. I lNVENkOR' m fM ATTORNEYS inc-48 April 1953 F. s. TUTTON PRODUCTION METHOD AND APPARATUS 4 6 w m 1 w W 77 7 d W m FL F FIG.59

Filed Dec. 27, 1946 Patented Apr. 28, 1953 UNITED stars 7 Claims. 1 The invention relates to a production method and apparatus for flowing wells.

This invention relates to the separation of well fluids in a well bore into one or more of their component parts and their subsequent ejection therefrom; a fluid recycling method in a well; control of the specific gravity and viscosity of formation fluids through the addition of heat energy and/or the products of. combustion by the apparatus hereinafter described; the regulation or formation pressures communicating with a well bore, through a controlled range of pressures from a normal negative valve to a positive quantity in the well bore; the subsurface transfer of the intrinsic energy, including free energy, (if an irreversible thermodynamic system employed in the production method of Wells hereinafter described; the intermittent pressurization and release of pressures in strata penetrated by a Well bore through the addition of fluids theretoby means of the combustion of a fuel-air mixture in one or more combustion chambers placed in the Well bore; the dissolution of minerals in a formation and their ejection to the surface, by means of heating a fluid in the well bore and its circulation into a formation as a result of the combustion of a fuel-air mixture in one or more combustion chambers placed in said well bore.

Certain substances and fluids can exist in the formation which on production thereof it is desirable to separate in the most expeditious, economical and effective manner. This is true, for efz'ample, in oil \vells'where basic sediment, sand, water occur with the production of oil, and which it has been found can be separated therefrom by subjecting the fluids to an increase of temperatures and pressures thereon, and by the agitation of same. H

ihe specific gravity and the fluidity of the formation fluids can be increased by mixing therewith fluids having a higher specific gravity and a lower viscosity, and also, in the case of crude oil, can be accomplished to an extent through the addition of natural gases or lighter petroleum fractions agitated in the oil, absorpti onoccurring as the pressures and the temperatures are increased.

In lowering the specific gravity of a fluid composed of several elements, it has been foundthat .ijuid, This is true c f brines, water-sulphur, and

sulphur-water mixtures, other mixtures and emulsions and various compounds Oi. elements found thus in their natural state or are mixed, emulsified, or compounded with other fluids to facilitate commercial recovery thereof.

One of several factors in the production or sugh fluids, through means of the well bores there,- into, has been the effective application of energy in the Well bore at a point or points therein dependent on and determined by the mechanical condition of the well bore and theformation or formations in communication therewith, to accomplish efiective production of the formation fluids.

In order that thesubsurface transfer of intrinsic energy, including free energy, of the irreversible thermodynamic system employed the production method ofwells hereinafterdescribed can be accomplished, provision has been made for the securing in a well bore, as subse,- quently disclosed, of one or more combustion chambers into which a combustiblefueleair mixture is induced, ignited, and the resultant energy derived from the combustion of the fuel employed to flow said well or form such pressure, temperature and velocity changes in Well fluids therein, and said formations in communication with said well bore as to accomplish the objectives of the invention. As hereinafter dis.- closed, each type of a form of apparatus embodying the invention is designed to accomplish one or more objectives of the invention. The method of the invention is sufficiently flexible to provide a subsurface transfer of energy in theivell bore under all conditions of the operation of the apparatus in the well bore.

As disclosed above, combustion occurringin the well bore, as subsequently described, provides energy which can be supplied to any desired formation in communication with a ell bore, the method of application of the energy being dependent on the number of strings of secured in the well bore and other factors. By providing submergible combustion chambers and a novel method of applying the productsof cornbustion formed therein, the operator therepf pan pressurize formations in communicationwith the well bore for a period of time, store energyin a fluid therein, which can be utilized as effective energy to flow the fluids through the formatipn, and/or eject the fluids from the well'bore,

Where it is desired that the dissolution of minerals in the formation be accomplished, .and subsequently ejected from the well bore; a fluid such as water can be introduced into the well here and heated to a high temperature therein by means disclosed, dissolving the minerals as a result thereof. The fluids can subsequently be ejected from the well bore by providing a suitable means, such as tubings in communication therewith, energy to effect said fluid flows au mented by the action of apparatus as herein disclosed.

With the foregoing in mind, the present invention has been devised, and it is an object of the invention, for ready adaption to the conditions determined for the production of formation fluids from any particular well bore in communication therewith, irrespective of the character of fluids therein, of the area of said Well bore, and the depth thereof. It is adaptable also to adjust itself to varying conditions of flow in the well bore, to flow the well, to repressure or pressurize said formations, and subsequently extract the fluids therefrom, to heat the fluids in said well bore and, for any one of said conditions or combination thereof imposed in the Well bore, said apparatus is adaptable also to mixing and agitating said fluids in said well bore, and of controlling the temperatures and pressures therein over a wide range of conditions in the well, and of the introduction of products of combustion in the fluid in the well, or the formations penetrated by a Well bore; to increase the absorption of one fluid by another, or by a mixture of said fluids.

The invention also comprehends subjecting to high temperatures and pressures, elements whose molecular activity can be increased with an increase in temperature and pressure, and to introduce said elements into a fluid in a well bore or a formation penetrated by the well bore for the purpose of extracting therefrom other elements in the production of fluids from the formations. Thus, the free energy change where any given chemical change can occur in the system of the invention, such as the combining of nitrogen and CO and CO2 at high temperatures with other elements, is accomplished in other energies in transit resulting from the combustion of the fuel utilized in the well.

Another object of the invention is to provide a method and apparatus employing one or more combustion chambers in a well bore, operable separately or simultaneously through the introduction of air thereto and to supply thereto a suitable combustible, which can be the fluid produced from the formation penetrated by the well bore. or introduced into the combustion chambers from a foreign source to form a combustible mixture therein, and igniting same for the purpose of flowing the well.

Another object of the invention is to provide method and apparatus for the pressurization or repressuring of a subsurface stratum by and through the addition of the products of combustion singularly or in combination with other fluids, thereto at greater pressures and temperatures than those existing in the formation by means of apparatus such as that hereinafter described.

Still another object of said invention is to provide method and apparatus for the separation of a fluid in a well bore into one or more of its com onent parts by means of heating, agitating and introducing thereto another fluid, the products of combustion, or the products of combustion and other fluids.

mation through the addition of heat energy in the well bore derived from combustion therein.

A still further object of the invention is to provide method and apparatus for the separation of a fluid in a well into one or more of its component parts by means of heating same in the well bore.

Another object of the invention is to provide method and apparatus for decreasing the specific gravity and viscosity of a fluid in a well bore by liberating the lighter elements in said fluid through the application of heat energy in said well bore.

Still another object of the invention is to provide method and apparatus for the regulation of pressures existing in a well bore, tubing, casing, or open hole, from a normal negative value to a positive quantity, and for th controlling of same by means of one or more combustion chambers in a well bore of the character described.

It is also an object of the invention to provide method and apparatus for the subsurface trans fer of the intrinsic energy, including energy resulting from a chemical change resulting from heating a fluid in a well bore and/or the combining therewith of the products of combustion in the well bore containing one or more combustion chambers therein.

Another object is to provide method and apparatus for the intermittent pressurization and release of pressures in formations penetrated by a well bore by means of providing one or more combustion chambers in the well bore; to effect pressure and temperature changes therein to extract fiuids from the formation.

Still another and more specific object is to provide means for suitably regulating and propagating a flame in one or more combustion chambers in a well bore by regulating the amount of air flowing thereinto.

Another object is to provide in a well bore one or more combustion chambers, igniters therefor, and means for supplying electrical energy to said igniters to effect the combustion of an inflammable mixture in the chambers.

A further object is to provide a device including a velocity tube or tubes, communicating with and forming an outlet for a combustion chamber in a well, producing a controlling effect upon the influx of air and fuel and their subsequent mixture in inflammable proportions in said combustion chamber, their ignition and flame propagation therein.

Still another object is to provide means comprising a throttle mechanism in one or more combustion chambers in a well bore, said means being operable as a function of the flow of a fluid to control the passage of fluids to said chambers.

Other and further objects and advantages of the invention will be readily apparent when the following description is considered in conjunction with the accompanying drawings wherein:

Fig. 1 is a diagrammatic view of one form of the invention installed in a well bore and utilizing three concentric strings of tubing within the well casing;

Fig. 2 is a diagrammatic view of a second form of the invention secured in a well bore and using two concentric strings of said tubing within the well casing;

Fig. 3 is a diagrammatic view of a third form of the invention secured in a well bore and utilizing a single string of tubing within the well casing;

Figs, i and 5 are successive vertical sectional high'tension electrical current, for ignition p ll-- poses to the power unit 6 and the power unit I, in the well bore, as follows:

The ignition cable 5 is connected to a suitable source of electrical energy through the switch ID at the surface. This cable passes through the casing head 9 and thence passes downwardly to the respective power units.

The ignition cable 5 is connected electrically to the outer extremities of the electrodes of the igniters in the power units in the well bore in a suitable manner and continuity of insulation of the conductors in the cable is maintained throughout the length of the cable. Hence, the flow of electrical energy from the switch It is through the ignition cable 5 and the electrodes secured into the combustion chambers so that an electrical spark is formed within the combustion chambers to ignite an inflammable mixture therein, as will be more fully described hereinafter.

The electrical circuit is preferably completed by utilizing the tubing in the well bore as an electrical conductor and a ground wire In, secured to a well head tubing, may be used to assure an adequate ground of the one side of the electrical circuit at the switch 9.

The upper section of easing head 9 is secured to the lower section thereof in a suitable manner, and the well casing I secured thereto is also secured in the well bore as by means of cement therearound, in a conventional manner. The lower section of the casing head carries wing connections ill and 10', having communication with the interior of the casing head. The wing connection I is connected to pipe line 12 and valve I2 therein enables the control of fluid flow through this line to the well head. It seems apparent that this construction provides a passage communicating with the annulus formed by the casing i and the tubing 2. In a similar manner the wing connection H! is connected to pipe conduit 65 having valve I4 therein, a pressure gauge 28 being provided in the conduit. It is to be noted that the assembly just described is also shown in Figs. 2 and 3, and like reference characters are used to designate like parts.

Referring to Fig. l, the flow line at includes T connection 65 communicating with valve 30 and with upper T 68 which, in turn, communicates with valves 2! and 22. The pipe 55 is connected directly tothe valve 22.

In Figs. 1 and 2, the casing head 9 carries the four-way connection 54 to which the tubing 2 is internally connected. The pipe 14 is connected through valve I6 to the connection and the opposite opening in the connection com municates with the valve I and in turn with T 38 interposed between this valve and the valve 3. The T 38 also communicates through valve 29 with the pipe 18.

Referring again to Fig. 1, the four-way connection I9 is secured to the upper end of the four-way connection 54. The tubing 3 is internally connected to this connection I9 so that the pipe 8|, attached thereto, communicates through valve I! to the annulus formed by the tubings 3 and 4. Valve I8 is also provided in a line communicating with this annulus, and the opposite side of this valve is connected through T 83 and valve 2| to the line 64. The upper opening in the T communicates with valve 2b which is in turn connected to T 90 to which flow line I9 isattached. The downward opening in the T 90 is connected to the tubing 4 and by virtue of this construction fluid may flow to or from pipe line 19 and/or the valve 20 and the tubing 4 within the well.

In Fig. 2, the upper end of the four-way connector 54 is connected through coupling '93 to the T M! and the tubing string 3 is connected interiorly to communicate with the passage in this T. A pipe line 93 is connected through valve 35 to the T whereby ingress or egress of fluid to and from the tubing 3 is provided in this form of the invention. The ignition cable 5 passes from the drum Hi9 to and through a packing gland 99 in the T 48. It is intended by this construction that the cable -5 may be lowered into the well to effect ignition after which sustained combustion will maintain operation of the device while the cable may be withdrawn upon the drum I35.

As will more fully appear, the lower end of cable 5 may be detachably connected to the igniter means within the power unit 23. A supplemental cable 5', having a common connection with such igniter means extends downwardly to the power unit 25 and supplies necessary electrical energy thereto when the cable 5 is lowered into the well and the switch i0 is closed.

The power unit 23 shown in Fig. 2 is preferably constructed as shown in Figs. 19 and 20 while the power unit 25 of this embodiment is shown in detail in Figs. 54 and 55. A packer 24, of any suitable construction is provided between the tubing 2 and the casing l to form upper and lower chambers above and below such packer, a bottom hole valve 59, such as that shown in Fig. 16, being provided in this production assembly.

In Fig. 3, the tubing 2, in the well casing I in the well bore, is shown as including an air separator 51, as further illustrated and described in Fig. 46. A power unit 52, as shown in detail in Figs. 39 and 40, and as further described herein, is secured in the tubing string 2 below the separator 51. Reference is made to the fact that the separator 51 and the power unit 52 are interconnected by a section of tubing 633 of limited length. The fuel tubing 635 and fuel conductor tubing 2 form a continuous conduit for transmitting fuel from the separator 5i to the power unit 52. It is to be understood that provision is made for the installation of an additional power unit or units, where required. The collar 93, secured to the upper section of the casing head 9, is connected seriatim to Ts Hi6 and IE8, valve Hi9, and T 2B2. The tubing string 2 is connected to the interior of the collar 93 whereby there is a common passage upwardly from the tubing through the assembly just described. Flow lines 263 and 2% enter Ts I08 and 282 respectively, and the upper opening in the T 202 is provided with packing gland 99 for the passage of cable 5 as previously described in connection with Fig. 2.

Pipe connection 65 in this embodiment forms a continuation of the pipe line 2I9 to provide communication, through valve I4, with the annular chamber formed by the well casing I and the tubing string 2.

Referring again to Fig. 1, it is to be understood that the pipe connection 55 may selectively communicate with any of the annuli formed between adjacent tubing strings in the well bore. Also, the pipe connection 18, and the pipe connection I 9 can, likewise, communicate with the several 21111311 formed in the well bore and in the well ea It is therefore possible by means of the con- -or outlet er a mention. Triis arran"genien where various combin'ati source of lfl uido receiver {Pipe-connection 1 tion 'of'theirifiarfiiriable InI p to surface means in communication therewith-byw An upper section of the t struction heretofore described and fabricated front-fittings connection 55 with: (a) the atmosphere, (b) a'suitable 5 source of gas or -oth'e'r gaseom iiuidi-(c) the inlet ible and e ar'iable -fof' 'sei vir ig tifle variousrequii-ements in production ifi accordance vith the mimportance as those illustrated" elem, re stalled in af'well i The pipe connection 8| normally provides a conduit between th'e "miulus formed by the tubreceiver, or to the atmosphere. The pip g on uitbetweenthe annulus formed by' thltubingsu the annulus "fb'inied ca in -I an intothe 'wel y "ing and repressuring purposes by m ansof'eitlrer df these colineal-Lions 'although -fluid 'o'ws frein t-he weirbore-are-per- "missible throug he'se menses- Referring'ag'aint rywith the type of power units' designated a ntti th alll'lullls formed by the tubings 2 andf3; A combustible of a "suitablecharactefi such as a natural gas; petroleum, or derivatives thereof, is nermanyintro duced -in'to the annulus-formed by the'tubings renew in saidwell"bo're'"as by means of'gravity flow "or under selected pressurei"" The airhnd combustible are intermixed in suitable inflammable proportions and are ignited "in the temperatechambers-m-the power-units in the well bore by'meafisof said'electrical energy conveyed "thereto products of com ",thetubing'fl."""

' The"'ilu ids, for recycling purposes, including flow from the welhbore'fparfbeadmittedtd'the annulus formed" by tne w li asin 1- anawhe A" form of the power unit 6 of Fig. 1 is shown in detail in' fiigsf l to s-reclusive; In this unit the "tubing 2 1s secured td-a nangeff I a; andthis "flange is in t'urn secured -toa" t1'ibi'rf5: carrier "-II I whereby the unit assembly issupported "by "the tubing.

concentrically "fitt' I I5 b'etween the male pressure in thewell'boreinto the 'ub'ingcarrier'li l The ally eirtending cylinder intehe spider II4 comm power units, such nulus formed by the tubings 2 and 3. Passages :I29rextenduownwardly from the annular-passage .130 to join Ethel-lower chamberIBI therewith; =2.zIn:val:similar.;manner.'.:an upper section of the tubing 4 zJcar-ries ;the :-male end, and terminates aimiaipressurer connector I;2I;avzhich rests withinand forms a seal with the cone seat I22 ofthe scylinder tlz'i. Bassage li lfids formed by the spider :Hrand the tubingi l, and .communicateswith the :annulusrsformed bytthe upper sections of the tub- 1, angst-3r and II: Pas'sagezl43 alsou communicates .w he:downwardlynextendingfuel pipes I35 and r4214;or zwhich the latteresupplies fuel to a' lower power unitor unitsu :3: I, r eNor-mallyrairsis conducted through the annuus formed by the tubings 2 andl 3, and fuel moves downwardly through the: annulus formed ,by I the rsai-dmuhingsrt and A's will-;subsequently be where; fully. described, the awellhfiuids, and the products of combustion move upwardly. through the tubing o. h

SVf ThBEfiYliHdBI H2 i provided with a chamber I25, 'ewhich:.-contains the spider: I234 concentritcally thereinw 'The'legs'of sthe spider I 23v are se- 25 cured to the interior walls of cylinder; I IZin the s r chamber x1261 uThe f-spider 123.5carries a hub (therein which servesas a guide for the stemoi sv'alvie lu'ifigf'slidablycfitetherethrough. and carries waive spring 124;? retainedzin placebythe hub of cthevspid'er I23anduthe head Lof 'thevalve I25,

2 tinuation ofzthe'tubing 2.2

Thewlowertubinggctirrier I28 has the lower jet housingsllll concentrioallysecured thereto. This jeti 'housing I3=I- has -1-th8 jet.-'bodies I42 formed -therein-y2andfthe:electrodes20rigniters HM are 45 mounted in the combustion chamber I 45. The

-'-;ztubexz-I 89: forms :axpart iof the combustion chamt ber and interconnects the-lower jet1 housing It I uandithe u'pperj et honsing I ITIr-r- A 'throttlef.mechanism 1I50, subsequently described; eis-= conoentrically secured- 'in the base of theijet housing- I 3.I--;.1 prior to the assembly of the 'fet housing' with -the lower tubing Jcarrier'IZS."

A co'nical tube -Iiid is secured to-the upper jet housings! ll and to the lower' end of the velocity tube l59Pup0nWhieh thevalve I25 seats as" a1- 'ready described. The valve I25 tends to remain sea ted u'pon the velocity tube 'I 5% due to thecomt pr'ession'of the valve spring I 26? The lower 'jets housings I3I has ports I33 60 formed -therein, said ports providing communica- 3 tion to the interior-of the carrier I31 and'to the nulus ltl-I as follows: 1 I

The power unitmasing I 21 is secured to the lowerend of the upper tubing carrier III. The

"peer fluid "separator tube i-l l-hhas its opposite e 'upper je't housing- I I I 7. and he cyIiHder-IIZ Thealupperiand lower jet housings II? and I3! are interconnected by-Ic'oncentri'cftubes v I89 and m'z I'liztto form ran-tannulus Hil ier "t'heipa'ssageiof swell fluids upwardly to: theLlcha-mber I-Zfifrom the passage]. Sfizferrh'ed in thezi-wails offthe lower "he :tubee I l- I:; the jet housings the; separator: tube IIILcooplie with the surroundingacasing I27 tosiorm the chamber I8I which is in effect a continuation of the annulus formed by the tubings 2 and 3. Passages I29 formed in the body of the upper tubing carrier III provide communication from the passage I30 previously described, to the annulus The chamber I8I communicates through ports 4I4 with the annulus H7, in the lower tubing carrier I 28, formedby the tubing carrier and the sleeve I18 which fits slidably upon the reduced upper end of the lower section of the tubing 3. The sleeve I18 is constantly urged upwardly by compression spring I19 to maintain a seal between the lower section of tubing and the lower tubing carrier I20.

The lower tubing carrier I28 interconnects the power unit casing I21 and the flange connection I80 which is in turn secured to a lower section of the tubing 2.

The lower section of the tubing 4 has a disconnect sleeve I60 at its upper end and this sleeve is constantly urged upwardly by the spring I01 into sealing engagement with the lower tubing carrier I28.

Ports I08 in the carrier I28 cooperate with passages I60, I10, I69 and I10 in sequence to conduct fluids from the lower portion of the tubing string 4 to the chamber I and thence to the bore of the upper portion of the tubing or flow string 4 for removal from the well bore as will be further explained.

The fuel pipe I conducts fuel downwardly to spaced metering valves I through which the fuel is introduced respectively to the lower and the upper jet carriers I3I and Ill. Similarly, the fuel pipe I15 conducts fuel downwardly to the passages I32 and I16 in the tubing carrier I28. Fuel conducted through the passage I15 is discharged into the annulus I14 for downward flow and use in a succeeding power unit or units. The fuel flowing through the passage IE2 is discharged into chamber I63 in the tubing carrier I28 for use in a manner that will presently appear.

' A Venturi body I34 is secured in the interior of the jet housing carrier I3I and has a wall port I13; with which the Venturi tubing I13 communicates to serve a purpose more fully explained in the description of Fig. 13 hereinafter.

To describe the operation of the device and supplement the description thereof, it is further explained that air moves downwardly through the annulus formed by the upper section of the tubing 2 and tubing 3, and the passages I30 and I20 and thence into the annulus I8I. A portion of the air is diverted through the ports I33, in the jet housing carrier I3I, as by moving from a high pressure area to that of a lower pressure area formed as subsequently described. The remainder of the air passages through the ports M4 to be conducted downwardly for use in lower power units as above explained.

That portion of the air stream diverted through the ports I33 moves over the throttle mechanism I thence through the Venturi body I34, and into the interior of the jet housing carrier I3I, having the fuel-air chamber I32 therein. Air in the chamber I32 is mixed with fuel supplied thereto through the jets I42 to form an inflammable fuel-air mixture within such chamber.

Fuel introduced to the annulus formed by the concentric arrangement of tubings 3 and 4 flows as by gravity through the passage I43 to the fuel metering valves I40, and thence to and through annuli MI and MI to the jets I42 and I42 whereby the metered fuel is introduced to the mixing chamber I32 and the combustion chamber I45.

It is understood, of course, that the introduction of air and fuel to the mixing chamber I32 shall be so coordinated as to provide an inflammable mixture. The inflammable mixture in the fuel-air chamber I32 moves upwardly through the mixing screen I8! secured to interior walls of the jet housing carrier I3I and is thus agitated whereby uniformity of the mixture is assured. The inflammable mixture thence passes over electrodes I45 in the combustion chamber I45 and is ignited therein as by means of an electric arc formed by energy supplied through the cable 5. The mixing of the fuel and air in the fuel-air chamber I32 is a continuous process, compression of the fuel-air mixture being achieved by the counter flow of the fuel and air thereinto.

The movement of the fuel-air mixture from the fuel-air chamber I32 to the combustion chamber I45 is caused initially, and at low pressures and temperatures, by the impact of air entering through the Venturi body I34. The character of the flame in the combustion chamber is similar to that of a torch. Where fuel and air pressures are rapidly increased, several phenomena occur depending on the character of fuel used and configuration of the combustion chamber. One phenomenon is that as the flame speed approaches the inherent combustion chamber resonance point, it results in rapid pressure fluctuations in the fuel-air mixture due to the nature of its compressibility, and also in the creation of a low pressure area at the base of the flame due to the rapid expansion of the gases of combustion. This low pressure area can be moved longitudinally in the combustion chamber as a function of fluid flows in the mixing and combustion chambers I32 and I45. Therefore, the point in the apparatus at which combustion starts to occur, the base of the flame, is controlled primarily by limiting the supply of oxygen, hence, in this instance, air flowing through the venturi I34, and over the automatic throttle mechanism I50, the functioning of which will now be generally explained. A more specific explanation is had in the description of Fig. 23.

That portion of the air entering ports I33 and which moves through the Venturi I34, flows over an air foil comprising a part of the throttle piston I5I in the throttle mechanism I50 protruding into the air passage formed by the ports I33 in the jet housing carrier I3I. The piston I5I fits slidably and rather loosely in the base of the jet housing carrier I3I to preclude its freezing thereto at high temperatures, and its freedom of motion is further insured by the spring I52 on which it rests.

As air velocities through the ports I33 are increased, a low pressure. area is formed along the sides of the throttle head I5 I which is fitted into the throttle piston I51. The throttle head and the throttle piston will thus tend to move as a function of velocity flows and their inherent weight, due to the formation of an air foil created by the movement of air flowing thereover.

Stops I53 are provided to preclude the momentum of slidable parts in the throttle mechanism I50, under some circumstances of operation, from thrusting themselves into the Venturi I34, thus closing the ports I33.

A central aperture I54 in the throttle head IBI 13 and the shank I41 thereo commuhieatss smith the chamber I56 therebelow whichg-inrturhacqm- :municates with portsz l M ,vpreviously idcsfiribed by 'way of.-r,adial.passage1!.51. ;This-air.1&t -acqm- -.-parative higher pressure movesthrough :theapgrture I54 by the difference jII'BIiP-DIQSSLJIES 313117116 .-'extremities-of said passagerandremoves any ex- ;traneous material between the riet'nhousing 1.9.8 ;rieraIBI and ,the throttle piston-,I;5,,I,;-and resutls in further functioning of the throttlepis ten' PM as ai function of, the static; and; kinetic; forces of the air. moving. over: the air ioil: iormed at the ;:apex of .the throttle'head I6].

Apart of the fuel is introduced intog-theipower through the, aperture I54; sincethe passage I 62in the lower tubing carrier 1 28; communicates 'lwith the' chamber I 63, formed in the, base of:-.the 4 throttle piston I 5 I andqthe: jet; 1housing carrier I3 I. A needle valve, assembly; is- -mounted in; the chamber I63;.and the needle thereof, is adapted .to slidably entertheopening' I641. 111.: the :bas o :A the throttle piston.

The throttle piston I5I is slidablyglout nonasotatablymo nted withinsthe. i t housiheloarri .I3I: as by means of key I83 on the throttle piston -.moving within complementary keyway I84 inthe acarrier.

:Ituis observed that. the thrott e-mechan sm L ;.obviates certain calculations in size-determina- -;tions of the venturis; ,such as 'venturi I3 4, ;and zthus increases: theutil-ityrof thepower unit. As

described above, the throttle mechanism I50 operates in proportioning of air to the power units in a system; compr sin one o mo e t .;,power units installedv in the-well bore.

. Combustion chamber 155-, formed as described, scommunicates with the velocitytube-I through which the products of combustion flow -inzexpanding. 'Ihesegasesthen pass into-the chamber .126 -which communicates with the tubing 4.

Thevelocity flo o t e produot oicomhus i engendered by the expansion ofthe products of combustion in the velocity tube 1 I 59 compresses the. spri y m hsine on t eheadhfsth .yalve I25; lightly retained ,,o n its seat -in the upper extremity of the velocity tube I 59;,by thespring I24,; as the kinetic energy of:theripmdusts of combustion exceeds vthe static pressure of the :nsp l 2 Well fluids nterthe power. un hrou h. a lower a section of the tubing 4;;due gto their hydrostatic .head or to the actionengenderedbya lower power rinitin thewell. such fluids ;move; upwardly ,throughjthe, ports I,68; and the apertures,..lfi9 ,to

i tlience into the mixing pharnber I25 over, the ,fins I I5, secured as by welding to the outersurface ':of-theveloc ity tube I59.; Thefins [.56 are formed :in a' vertical spiral-direction relative. toytheve- ;-;locity tube 159, teincrease the surface area there- 1-1011. exposed. to; the well v,iiuids and to limit lateral movement ofgthe velocity tubed 59.

1 Due to energy relationships; previously-dis closed --:.and further described herein; we1l;-fluids arepro- ;p elledpfrom jthemixin' chamber ;I 26 through. the 5 :upper. section. of the tubing tandrthence to sur- .1 stacemeansdn communication therewith,.by aera- 5 tionfof, the, wellfiuidsandthe expansion of:.the igases thereindue to .commingli-ng'of the products 301 combustion inexpanding toatmospheri-c pres- -..sure.

venturi pressure, as aiunction Ofwthfiil flow mthrough the venturi 134, is-transmittedto theflfuel metering valves 'l fifl from the apexsof theventuri I 3 liby meansor port I I3 formed' thereinand in i 55. 2II is secured tof thetu trated has contemp ,tio wi h the inv n ion; t Qhs ru trically therein and formed -;.thereof,,aspiderinto whichv I 2I5 ,efiects the seal I M-therewith. due; to-.-the

t ng. 3 smsuificient tosse b n sen-b secured- -rier 2 I0 as by ihleads.

. h pressure and fuel pressures o 1385311184116 I t in v lve as .dess b zi. ne :flsile in Fig. 13, toefiect fpropo hing o the iuel to orm a combust e xtu wiih thes flowin into-thefuel-air chamberand the combustion cham e I is b e ed i a siha th QQII P IQ Q 'i1 P ts he e r gh o m tehis rials under.wor in ;t m erat re.r iisi sh f rm o o st t o smb ihet i'e 90. cen ric s n s of; tubin c th owsrun referred to as the power unit: 1; 1- Fig.1, oras the bottom hole power unit, th e well bore containngthe wel casi g 1 uh hes ;;3 end 5 11. 15 illustrat di F s-fiend V The same character references previouslyema ed f t ere pes v str hes-of'tu nain the -well borearerepeatqd .he eih an dflth sa ne character reference for -the ignition cabl well casing I,as illustratedp" a'pdfi a e e eate a in. spe ific. eierehs he ei i als meet Figs. 4 andi5.

For the purpos .achievih rrehiaiemili riea- .h apparatus; as illustrated Rigs; 9 and l 0 is described as follows:

he fl n 2 3 shown in Ei ..i .secursdso t bin 2 an rc r e tubinahousihearr 2!" secured here a by,- means f. .stu 'holt 1. threaded into the body .of the tubing: using r e 2 at t rvalsie eue t e; b sl sr thereof. I

The tubing housing carrier; 218 i secured to power unit casing L92 as by means of a n external extrusion on said power ;unitca ing inthejorm h a n e formed as e lihteer lrs there The power unit casing I92 carries swage nipple I a its lower e r mit pehdrt e.whines is secured-theretqas .by th d T -8 mentioned.

Th t bin hou inebsrrisr 2W nts 'r .1 sur c n ect o fected by the weight of thetubingr l onthecone seat ;I- 22. ;.-W'here the weight ,of the tubing 4 is ns fi i nt-to f r /.efi tive ythe/de ribed. se

.. -W th tubing housing carrier-.11 athe tubing 4 can be secured to the tubing housing carrier glfl a i rme nsorthread v v nicate withthe annulu 2% therein the fluid separator tube' 2 2fi secured ,tofthe t b n ho s bar ier? flhetu ellz s fur- 70.

. the power unit. casing e. rene al fitt h r ec re vflat scre s?" u the; sp der 7 24! therein and'tb wh ch the lower. egrtjremi tyof velocity tube assembly?ll flis' secured as 55; weresecured to velocitytube izfli 

